Author

E. Ann Bare

Observed names: Bare, E. A., Bare, E. Ann, Bare, E. Ann., E. A. Bare, E. BARE, E.A. Bare

Observed institution: Langley Research Center

OpenAlex ID: A5013242533

The NASA Langley 16-Foot Transonic Tunnel---Historical Overview, Facility Description, Calibration, Flow Characteristics, Test Capabilities

1995 · F. J. Capone, Linda S. Bangert, et al. · NASA Technical Reports Server (NASA) · 19

Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters

1989 · E. A. Bare, F. J. Capone · NASA STI Repository (National Aeronautics and Space Administration) · 11

An embedded wireless data acquisition system for wind tunnel model applications

2002 · E. Adcock, J. Bartlett, et al. · International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF) · 8

Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20

1992 · F. J. Capone, R. J. Re, et al. · NASA Technical Reports Server (NASA) · 7

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Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47

1987 · F. J. Capone, E. A. Bare · NASA Technical Reports Server (NASA) · 7

Subsonic/supersonic aerodynamic characteristics for a tactical supercruiser

1984 · F. CAPONE, E. BARE, et al. · AIAA Applied Aerodynamics Conference · 5

Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring

1987 · E. A. Bare, D. E. Reubush · NASA Technical Reports Server (NASA) · 4

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The impact of LO-configured forebodies on inlet approach flowfields

1991 · RAYMOND HADDAD, DONALD BINGAMAN, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 3

Parametric study of single expansion ramp nozzles at subsonic/transonic speeds

1987 · F. CAPONE, R. RE, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 3

Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics

1983 · L. D. Leavitt, E. A. Bare · University of Michigan Library Repository · 3

Thrust reversing effects on twin-engine aircraft having nonaxisymmetric nozzles

1981 · F. CAPONE, R. RE, et al. · AIAA/NASA Ames V/STOL Conference · 3

Effect of simulated in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models. [conducted in the Langley 16-foot transonic tunnel]

1981 · E. A. Bare, B. L. Berrier, et al. · NASA Technical Reports Server (NASA) · 3

Flowfield investigation of a supercruise fighter model

1985 · David E. Reubush, E. Ann Bare, et al. · Journal of Aircraft · 2

Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics. [Langley 16-ft transonic tunnel tests]

1983 · L. D. Leavitt, E. A. Bare · NASA Technical Reports Server (NASA) · 2

Effect of simulated in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models

1981 · E. A. Bare, B. L. Berrier, et al. · NASA Technical Reports Server (NASA) · 2

Parametric Study of Afterbody/nozzle Drag on Twin Two-dimensional Convergent-divergent Nozzles at Mach Numbers from 0.60 to 1.20

1986 · Odis C. Pendergraft, James R. Burley, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 1

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Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle

1987 · George T. Carson, E. A. Bare, et al. · University of Michigan Library Repository

Investigation of a delta-wing fighter model flow field at transonic speeds

1987 · E. BARE, DAVID REUBUSH, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Investigation of a supersonic cruise fighter model flow field

1985 · D. E. Reubush, E. A. Bare · NASA STI Repository (National Aeronautics and Space Administration)

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Flow-field investigation of a supercruise fighter model

1984 · D. REUBUSH, E. BARE, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds

1983 · E. A. Bare, Odis C. Pendergraft · NASA STI Repository (National Aeronautics and Space Administration)

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Investigation of installation effects on twin-engine convergent-divergent nozzles

1983 · E. A. Bare, B. L. Berrier · NASA STI Repository (National Aeronautics and Space Administration)

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Effect of nozzle and vertical-tail variables on the performance of a 3-surface F-15 model at transonic Mach numbers

1982 · Odis C. Pendergraft, E. A. Bare · NASA Technical Reports Server (NASA)

Effect of nozzle and vertical-tail variables on the performance of a 3-surface F-15 model at transonic Mach numbers. [Langley 16 foot transonic tunnel]

1982 · Odis C. Pendergraft, E. A. Bare

Works count: 42

Citation count: 83

H-index: 5

I10-index: 2